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04-BS-7 · May 2016

Question 4 of 13: Minimum Wind Velocity to Lift a Flat Insulation Panel

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

04-BS-7 Mechanics of Fluids — May 2016 (National Examinations, three hours, closed book). Section A (Calculative) offers 9 questions and instructs "do seven"; Section B (Analytical/Graphical) offers 4 questions and instructs "do three." Every question is answered below (13 of 13), so students can use the full paper as a study resource. Constants used throughout (from the paper's own Constants page): g = 9.81 m/s², patm = 100 kPa (an atmospheric head of 10 m of water is specified separately for Question 1), ρwater = 1000 kg/m³, SGglycerine = 1.26, SGmercury = 13.56, ρconcrete = 2400 kg/m³, ρair = 1.19 kg/m³ (20°C) / 1.21 kg/m³ (15°C), μwater = 1.0×10⁻³ N·s/m², Rair = 287 J/kg·K.

Reference texts: F. M. White, Fluid Mechanics, 8th ed. (McGraw-Hill) — fluid statics and manometry (Ch. 2), hydrostatic forces and the middle-third rule (Ch. 2), dimensional analysis and drag (Ch. 5, 7), pipe friction and the Moody/Colebrook relation (Ch. 6), control-volume momentum (Ch. 3); B. R. Munson et al., Fundamentals of Fluid Mechanics — jets, orifices, and streamline patterns (Ch. 5, 8); J. D. Anderson, Fundamentals of Aerodynamics — wave/compressibility drag divergence (Ch. 5) for the Boeing 747 wind-tunnel chart used in Question 9.

Question 4: Minimum Wind Velocity to Lift a Flat Insulation Panel (5 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given.

QuantityValue
Panel size2.438 m × 1.219 m × 25 mm thick
Panel density ρp100 kg/m³
Underside conditionstagnation (grass reduces velocity to zero)
Ambient air density ρair (assumed 15°C)1.21 kg/m³

Find. The minimum wind velocity V (km/hr) that lifts the panel.

Check: the paper gives air density at both 20°C and 15°C; 15°C (1.21 kg/m³) is used here as the ambient reference — using 20°C instead changes the answer by under 1%.

Approach. Apply Bernoulli along the streamline that reaches stagnation under the panel (pressure there = Patm + full dynamic pressure) and compare with the pressure just above the panel, where the wind still moves at essentially the free-stream velocity V (pressure there ≈ Patm); the panel lifts when this pressure difference times its area equals its weight.

  1. Pressure difference across the panel. Below (stagnation): $p_{below}=p_{atm}+\tfrac12\rho_{air}V^2$. Above (undisturbed free stream at the same elevation): $p_{above}=p_{atm}$. So the net uplift pressure is $$\Delta p = p_{below}-p_{above} = \tfrac12\rho_{air}V^2$$
  2. Set uplift force equal to panel weight. Panel weight per unit plan area is $\rho_p g t$ (t = thickness), so at lift-off: $$\tfrac12\rho_{air}V^2 = \rho_p g t \quad\Rightarrow\quad V=\sqrt{\frac{2\rho_p g t}{\rho_{air}}}$$
  3. Substitute numbers. $$V = \sqrt{\frac{2(100)(9.81)(0.025)}{1.21}} = \sqrt{40.54} = 6.37\ \text{m/s}$$ $$V = 6.37 \times 3.6 = \boxed{22.9\ \text{km/hr}}$$
QuantityResult
Minimum lift-off wind velocity V6.37 m/s = 22.9 km/hr